Robinson Helicopter Company R44 II accident near Chugiak, Alaska, May 28, 2014
On May 28, 2014 at about 10:33 pm local time, a 2006 Robinson Helicopter Company R44 II, registered N392GP, was destroyed in an accident during maneuvering near Chugiak, Alaska (Birchwood airport). It was an external-load flight under external-load helicopter rules (Part 133). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's loss of control of the helicopter due to impairment or incapacitation from a sudden, acute cardiac event.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 28, 2014 · about 10:33 pm local time
- Place
- Chugiak, Alaska · Birchwood · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Robinson Helicopter Company R44 II, built 2006
- Registration
- N392GP · no longer on the register · serial 11238
- Damage
- Destroyed
- Flight
- External-load flight · external-load helicopter rules (Part 133)
The NTSB's narrative final · quoted from the NTSB record
***This report was revised on November 29, 2017. Please see the docket for this accident to view the original report.*** The accident flight was one of several recent practice external-load flights that the pilot had been conducting with a 150-ft long-line and weighted barrel. The helicopter approached the airport from the north and then hovered over the approach end of runway 20R. At the time, two airplanes were in the airport traffic pattern for runway 20R, another was in the airport vicinity, and a fourth was departing from runway 2R toward the hovering helicopter. One witness reported hearing the accident pilot attempt to communicate with the departing northbound airplane, but no response was heard, and the airplane passed close to the helicopter. After the northbound airplane passed by, the helicopter moved to its normal landing area on the east ramp, and the accident pilot responded to another pilot's query as to his intentions by stating that he was landing. Immediately after the pilot's response, the helicopter suddenly pitched up, rolled left, and descended to the ground. Examination of the helicopter revealed no evidence of preimpact mechanical anomalies with the airframe, systems, or powerplant. Damage to the main rotor and associated ground scars and wreckage distribution were consistent with the rotor system operating at normal rpm during the impact sequence. Damage to the helicopter and the location of the main rotor ground scar were consistent with the helicopter having collided with the ground in an extreme left roll. The long-line remained attached to the barrel but was not attached to the helicopter's cargo hook, and the disconnected end was near the main wreckage. The relative orientation of the long-line and the main wreckage indicated that the line was still attached to the helicopter when the helicopter moved laterally at some point; however, no known witness observed when or how smoothly the line and load were released. Maneuvering a helicopter to land during external load operations requires precision in both helicopter control and timing of load release. Although the accident pilot's workload was increased by the demands of maintaining traffic separation and communicating on the radio in the busy, nontowered airport environment, there was no evidence to suggest that such an operation was beyond his skill level, particularly given his recent practice. The accident pilot was based at BCV and, in the 2 weeks before the accident, had conducted seven flights (including the accident flight) with a 150-foot long-line in the accident helicopter; in the preceding 90 days, the pilot had flown almost 60 hours, most of which involved autorotations, hover maneuvers, and long-line practice. The pilot's autopsy identified severe coronary artery disease with greater than 75% stenosis in two main arteries. In addition, scarring in the left ventricle was identified, which indicated that the pilot had experienced a previous heart attack. Although the pilot had sought and received in recent years medical care that included cardiac testing, there is no evidence that his previous heart attack was ever diagnosed (research has shown that the tests are not always accurate). Given the presence of two severely stenotic lesions in two main arteries and the presence of scarring from a previous heart attack, the accident pilot's likelihood for experiencing another acute cardiac event (such as a new heart attack, anginal symptoms, or an acute arrhythmia) was inevitable. An acute cardiac event would likely cause symptoms ranging in severity from impairing (such as chest pain and shortness of breath or palpitations) to incapacitating (fainting from low blood pressure or sudden cardiac death). Further, such an event occurring immediately before impact would likely leave no identifiable evidence on autopsy. Considering the precision required while maneuvering to land with an external load, any level of impairment could result in catastrophic consequences; therefore, the pilot likely experienced a sudden, acute cardiac event that adversely affected his performance.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- External load event (Rotorcraft) during maneuvering defining event
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Personnel issues › Physical › Health/Fitness › Predisposing condition › Pilot
- cause Personnel issues › Physical › Impairment/incapacitation › Cardiovascular › Pilot
Pilot
- Certificate: commercial pilot
- Ratings: rotorcraft: helicopter
- Flight time: 2,174 hours in all; 59.5 in the last 90 days; 25 in the last 30 days; 2,061.3 as pilot in command
- Last flight review: July 1, 2013
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 2,320.2 hours
- Last inspection: type not recorded, March 14, 2014
- Maximum gross weight: 2,500 lb
- Landing gear: fixed
- Engine: Lycoming IO-540 SER (piston); 0 hours total
- Fire on the ground
- Operator: Global Positioning Services INC
The flight
- Departed from: BCV Chugiak AK
- Destination: BCV Chugiak AK
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 300° at 3 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 7,000 ft
- Temperature: 57°F (14°C), dew point 43°F (6°C)
- Altimeter: 30.10 inHg
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
Other NTSB records under N392GP the same tail number, which may have belonged to a different aircraft at the time
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
